Crack initiation mechanism in a high-strength Ti-5Al-7.5V alloy subjected to high cycle fatigue loading-Reference-Cited by-同舟云学术

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Crack initiation mechanism in a high-strength Ti-5Al-7.5V alloy subjected to high cycle fatigue loading

Published:2023-06 Issue: Volume:148 Page:107201
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Wu Zhihong,Kou Hongchao,Chen Nana,Qiang Fengming,Fan Jiangkun,Tang Bin,Li Jinshan

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference54 articles.

1. Williams, Edgar A;James;Starke, Jr, Progress in structural materials for aerospace systems, Acta Mater.,2003

2. Determination and analysis of the cyclic and dwell fatigue performance of TIMETAL 575;Thomas,2016

3. Air Force Office of Scientific Research;Chang,1996

4. Titanium alloy developments for aeroengine fan systems;Hewitt;Mater. Sci. Tech.,2014

5. Fatigue crack initiation on slip bands: Theory and experiment;Lin;Acta Metall.,1986

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